FIELD AND BACKGROUND OF THE INVENTION
[0001] The present invention relates to alignment of antenna polarization axes and, in particular,
it concerns alignment of antenna polarization axes of a dual polarized end-user terminal.
[0002] Geostationary satellite transponders are in common orbit 23,000 miles above the earth.
The satellites share common latitude on the equator and are spaced apart longitudinally
in an orbital arc, called the Clark belt, sometimes by less than one degree. When
communicating with these satellites care must be taken not to illuminate more than
one satellite with up-link radio frequency energy and, conversely, not to receive
interfering signals from adjacent satellites located along the Clark belt. A satellite
communicates using various frequencies to maximize the communication capacity of the
satellite. Moreover, a satellite also typically communicates in two polarization axes,
being orthogonal to each other, to maximize the capacity of each available frequency.
Regulatory authorities, such as the FCC and ETSI require that the end-user terminal
be aligned very accurately with the satellite. The regulations require that other
satellites and also a non-designated polarization axis of the designated satellite
will not receive even a component of the transmitted signal from the end-user terminal
that exceeds a very low threshold. Therefore it is essential for the azimuth, elevation
and polarization alignment of the end-user terminal to be aligned accurately. As is
known in the art, azimuth and elevation alignment can be performed by adjusting the
antenna direction of the end-user terminal to maximize the received signal from the
designated satellite. This is known as the signal strength pointing method. Similar
adjustment for polarization alignment does not yield satisfactory results and another
method must be, employed. The current method for polarization adjustment includes
the installer sending a linearly polarized test signal from the end-user terminal
to the satellite. The test signal is received by the satellite. A component of the
test signal is received in one polarization axis of the satellite and another component
of the test signal is received in the other polarization axis of the satellite. The
magnitude of the components in each axis is received by the satellite control center.
The installer telephones the control center for the results and then adjusts the antenna
polarization. Another test signal is sent to the satellite and the process continues
until the antenna polarization is aligned with the satellite. This process is very
difficult, time consuming and not accurate. Moreover, the designated frequency in
both polarization axes of the satellite cannot be used for normal communications during
this alignment process.
[0003] Document EP 1 303 002 discloses a method for the polarization alignment of an antenna
of an earth station with the polarization axis of the antenna of a satellite by processing
the satellite beacon signal in order to get a measure of misalignment.
[0004] Document US 5 568 158 describes electronic circuitry which adjusts the polarization
of an antenna feed to match the polarization of an incoming signal in order to maximize
the signal to noise ratio.
[0005] There is therefore a need for a system and method of aligning antenna polarization
axes of a dual polarized end-user terminal.
SUMMARY OF THE INVENTION
[0006] The present invention is a system and method of aligning antenna polarization axes
of a dual polarized end-user terminal.
[0007] According to the teachings of the present invention there is provided, a method for
aligning antenna polarization axes of a dual polarized end-user terminal having an
antenna, the antenna being aligned with a satellite in relation to azimuth and elevation,
the end-user terminal being configured to produce a first output corresponding to
a first component of a received signal parallel to a first polarization axis of the
antenna and a second output corresponding to a second component of the received signal
parallel to a second polarization axis of the antenna, the first polarization axis
being orthogonal to the second polarization axis, the method comprising the steps
of: (a) receiving a linearly polarized signal having a frequency wherein for the frequency
and during a time period when the signal is being transmitted, the satellite is not
transmitting signals with a linear polarization that is orthogonal to the linearly
polarized signal; (b) autocorrelating first output and the second output such that,
only correlating terms of the first output and the second output are multiplied together
producing a measurement of autocorrelation; and (c) adjusting the antenna polarization
axes to minimize the measurement of autocorrelation.
[0008] According to a further feature of the present invention, the step of autocorrelating
is performed by inputting the first output and the second output into an electronic
mixer to produce the measurement of autocorrelation.
[0009] According to a further feature of the present invention, there is also provided the
step of reducing proportionately frequencies of the first output and the second output.
[0010] According to a further feature of the present invention, there is also provided the
step of tuning the first output and the second output to the frequency.
[0011] According to a further feature of the present invention, there is also provided the
step of filtering the first output using a first band pass filter and the second output
using a second band pass filter.
[0012] According to a further feature of the present invention, the step of autocorrelating
is performed by inputting the first output and the second output into an electronic
mixer and inputting the output of the electronic mixer into a low-pass filter to produce
the measurement of autocorrelation.
[0013] According to a further feature of the present invention, there is also provided after
the step of autocorrelating, the step of displaying the measurement of autocorrelation.
[0014] According to a further feature of the present invention, the step of adjusting is
performed by actuating an alignment actuator configured to adjust the antenna polarization
axes to minimize the measurement of autocorrelation.
[0015] According to the teachings of the present invention there is also provided, a system
for aligning antenna polarization axes of a dual polarized end-user terminal having
an antenna, the antenna being aligned with a satellite in relation to azimuth and
elevation, the end-user terminal being configured to produce a first output corresponding
to a first component of a received signal parallel to a first polarization axis of
the "antenna and a second output corresponding to a second component of the received
signal parallel to a second polarization axis of the antenna, the first polarization
axis being orthogonal to the second polarization axis, the system comprising: (a)
a first connection configured for connection to the end-user terminal for receiving
the first output; (b) a second connection configured for connection to the end-user
terminal for receiving the second output; and (c) an autocorrelation apparatus having
a first input and a second input; said first connection being connected to the first
input, said second connection being connected to said second input, said autocorrelation
apparatus being configured for autocorrelating the first output and the second output
such that only correlating terms of the first output and the second output are multiplied
together producing a measurement of autocorrelation.
[0016] According to a further feature of the present invention, the autocorrelation apparatus
includes an electronic mixer having a first input that is connected to the first connection
and a second input that is connected to the second connection.
[0017] According to a further feature of the present invention: (a) the autocorrelation
apparatus further includes a low-pass filter having an input; and (b) the electronic
mixer has an output that is connected to the input of the low-pass filter.
[0018] According to a further feature of the present invention: (a) the low-pass filter
has an output; and (b) the input of the display is connected to the output of the
low-pass filter.
[0019] According to a further feature of the present invention: (a) the autocorrelation
apparatus further includes a dual polarized block down-converter having a first input
that is connected to the first connection and a second input that is connected to
the second connection; and (b) the dual polarized block down-converter is interposed
between the first connection, the second connection and the electronic mixer.
[0020] According to a further feature of the present invention, there is also provided:
(a) a first down-converter that is interposed between the first connection and the
electronic mixer; and (b) a second down-converter that is interposed between the second
connection and the electronic mixer.
[0021] According to a further feature of the present invention, the autocorrelation apparatus
includes: (a) a first tuner that is interposed between the first connection and the
electronic mixer; and (b) a second tuner that is interposed between the second connection
and the electronic mixer.
[0022] According to a further feature of the present invention, the autocorrelation apparatus
includes: (a) a first band pass that is interposed between the first connection and
the electronic mixer; and (b) a second band pass filter that is interposed between
the second connection and the electronic mixer.
[0023] According to a further feature of the present invention, there is also provided an
alignment control system and an alignment actuator wherein the alignment control system
is configured to control the alignment actuator to adjust the antenna polarization
axes in response to an output of the autocorrelation apparatus.
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] The invention is herein described, by way of example only, with reference to the
accompanying drawings, wherein:
Fig. 1 is a schematic orthogonal view of a linearly polarized signal being received
from a satellite by an end-user terminal in alignment mode that is constructed and
operable in accordance with a preferred embodiment of the invention;
Fig. 2 is a schematic plan view of the linearly polarized signal being received by
the end-user terminal of Fig. 1;
Fig. 3 is a schematic view of an alignment equipment setup for use with the end-user
terminal of Fig. 1;
Fig. 4 is a schematic representation of the operation of an autocorrelation apparatus
for use with the end-user terminal of Fig. 1;
Fig. 5 is a table comparing the system of Fig. 4 to a signal strength system of polarization
alignment;
Fig. 6 is a schematic representation of the operation of an alignment control system
for use with the autocorrelation apparatus of Fig. 4.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0025] The present invention is a system and method of aligning antenna polarization axes
of a dual polarized end-user terminal.
[0026] The principles and operation of a system and method of aligning antenna polarization
axes of a dual polarized end-user terminal according to the present invention may
be better understood with reference to the drawings and the accompanying description.
[0027] Reference is now made to Fig. 1 and 2. Fig. 1 is a schematic orthogonal view of an
end-user terminal
10 receiving a linearly polarized signal
15 from a satellite
20 in alignment mode that is constructed and operable in accordance with a preferred
embodiment of the invention. Fig. 2 is a schematic plan view of the end user terminal
10 receiving linearly polarized signal
15. End-user terminal has an antenna
17. Antenna
17 includes a reflector
18 and an antenna feed
19. End-user terminal
10 is dual polarized meaning that antenna
17 has an associated polarization axis, known in the art as co-polarization axis
25 and an associated polarization axis, known in the art as cross polarization axis
30. Co-polarization axis
25 is orthogonal to cross polarization axis
30. End-user terminal
10 is configured to produce an output corresponding to a component of a received signal
parallel to co-polarization axis
25. End-user terminal
10 is also configured to produce another output corresponding to a component of a received
signal parallel to cross-polarization axis
30.
[0028] Before polarization alignment commences antenna
17 is aligned with satellite
20 in relation to azimuth and elevation. Polarization axes
25,
30 are aligned as close as possible with the polarization axes of satellite
20. Typically, this initial polarization is within 5 degrees of the optimal polarization.
The alignment process now commences. Antenna
17 receives linearly polarized signal
15. Signal
15 is transmitted at a known frequency. In fact, signal
15 is typically a modulated signal having a range of frequencies. Therefore, the term
frequency refers to a range of frequencies or frequency band. During the time period
of the alignment process it is important that for the frequency of signal
15, satellite
20 is not transmitting signals with a linear polarization that is orthogonal to the
linear polarization of signal
15. End-user terminal
10 produces an output
40 corresponding to a component
45 of signal
15 received parallel to co-polarization axis
25 and an output
50 corresponding to a component
55 of signal
15 received parallel to cross polarization axis
30. Output
40 and output
50 are autocorrelated and produce a measurement of autocorrelation. Output
40 and output
50 may contain signals and other than signal
15. Therefore, by autocorrelating output
40 and output
50, only parts of output
40 and output
50 that contain signal
15 will be multiplied together to produce the measurement of autocorrelation. Therefore,
the measurement of autocorrelation gives a measurement of the alignment of polarization
axes
25,
30 to the polarization axis of signal
15. Therefore, the measurement of autocorrelation gives a measurement of the alignment
of polarization axes
25,
30 to the polarization axes of satellite
20. As the polarization axis of signal
15 becomes more parallel to co-polarization axis
25, component
45 increases and component
55 decreases and therefore the measurement of autocorrelation decreases. When the polarization
axis of signal
15 is parallel to co-polarization axis
25, the measurement of autocorrelation will be zero. Polarization axes
25,
30 of antenna
17 are adjusted to minimize the measurement of autocorrelation. The above method of
alignment enables accurate and quick alignment of antenna polarization without the
need to send a signal to the satellite and to telephone the control center to receive
adjustment data.
[0029] Reference is now made to Fig. 3, which is a schematic view of an alignment equipment
setup
60 for use with end-user terminal
10. Alignment equipment setup
60 includes an autocorrelation apparatus
65 that autocorrelates output
40 and output
50. Autocorrelation apparatus
65 is explained in more detail with reference to Fig. 4. Alignment equipment setup
60 also includes a display device, typically being a digital voltmeter (DVM)
70, for displaying the measurement of autocorrelation calculated by autocorrelation
apparatus
65. Polarization axes
25, 30 are adjusted, typically manually, to minimize the reading of voltmeter
70. It should be noted the measurement of autocorrelation could be processed to enable
display by other methods and these methods might not include the use of a digital
voltmeter to display the result. Alternatively, the output of autocorrelation apparatus
65 is directly connected to an alignment control system
75. Alignment control system
75 is configured to operate an alignment actuator
80. Alignment actuator
80 adjusts polarization axes
25, 30. Alignment actuator
80 is typically a system of fluid operated or motorized actuators that adjust at least
one of reflector
18 and antenna feed
19. Alignment control system
75 is explained in more detail with reference to Fig. 6.
[0030] Reference is now made to Fig. 4, which is a schematic representation of the operation
of autocorrelation apparatus
65. Autocorrelation apparatus
65 includes a dual polarized low noise block down-converter (LNB)
85. Block down-converter
85 typically forms part of end-user terminal
10 and is located close to antenna feed (FEED)
19. Output
40 and output
50 are inputs of block down-converter
85. Block down-converter
85 reduces proportionately all frequencies contained within output
40 and output
50 from Ku-band or C-band to L-band. Block-down converter
85 produces an output
90 corresponding to down-converted output
40 and an output
95 corresponding to a down-converted output
50. One output terminal of block down-converter
85 is connected to the input terminal of a tuner
100 and the other output terminal of block down-converter
85 is connected to the input terminal of a tuner
105. Output
90 is input to tuner
100 and output
95 is input to tuner
105. Tuner
100 tunes output
90 to the down-converted frequency of signal
15. Tuner
105 tunes output
95 to the down-converted frequency of signal
15. Tuner
100 and tuner
105 also down-converts the frequencies contained within output
90 and output
95 from L-band to IF-band. Tuner
100 produces an output
110. Tuner
105 produces an output
115. The output terminal of tuner
100 is connected to the input terminal of a band-pass filter (BPF)
120. The output terminal of tuner
105 is connected to the input terminal of a band-pass filter
125. Band-pass filters
120,
125 typically have a pass band that is in the range of 6 MHz to 8 MHz wide. Band-pass
filters
120, 125 reject unwanted noise received by antenna
17 at the edges of the frequency band of signal
15. Band-pass filter
120 produces an output
130. Band-pass filter
125 produces an output
135. The output terminal of band-pass filter
120 is connected to the input terminal of a variable attenuator
140. The output terminal of variable attenuator
140 is connected to the input terminal of a variable gain amplifier
145. The output terminal of band-pass filter
125 is connected to the input terminal of a variable attenuator
150. The output terminal of variable attenuator
150 is connected to the input terminal of a variable gain amplifier
155. Output
130 is amplified by variable gain amplifier
145 and adjusted in level by variable attenuator
140 to produce an output
160. Output
160 has a signal level in the range of 0 dBm to 15 dBm to comply with the working range
of a double balanced mixer
165 in the next stage of autocorrelation apparatus
65. Output
135 is amplified by variable gain amplifier
155 and adjusted in level by variable attenuator
150 to produce an output
170. Output
170 has a signal level in the range of 0 dBm to 15 dBm to comply with the working range
of double balanced mixer
165 in the next stage of autocorrelation apparatus
65. Double balanced mixers are commercially available, for example, from Mini Circuits,
Brooklyn, New York. The output terminal of variable gain amplifier
145 is connected to a first input terminal of double balanced mixer
165. The output terminal of variable gain amplifier
155 is connected to a second input terminal of double balanced mixer
165. Double balanced mixer
165 produces an output
175 that contains a low frequency component and a high frequency component. The low frequency
component of output
175 is proportional to the multiplication of correlating terms of output
160 and output
170. The high frequency component of output
175 is proportional to non-correlating terms of output
160 and
170 and to the multiplication of correlating terms of output
160 and output
170. The output terminal of double balanced mixer
165 is connected to the input terminal of a low-pass filter (LPF)
180. Low-pass filter
180 is typically in the range 1 Hz to 10 Hz. Low-pass filter
180 produces an output
185 that contains the low frequency component of output
175. Output
185 is therefore the measurement of autocorrelation of output
40 and output
50.
[0031] It should be noted that substitute components are typically available for use in
autocorrelation apparatus
65 to provide the same functionality as the components mentioned above. Moreover, the
components of autocorrelation apparatus
65 may be assembled in a different order and some may be omitted entirely. For example
if a higher frequency mixer is available it is possible to remove some or all of the
down-converters. In addition, the amplifiers and attenuators may not be needed.
[0032] The output terminal of low-pass filter
180 is connected to the input terminal of digital voltmeter
70 for displaying the measurement of autocorrelation calculated by autocorrelation apparatus
65. Alternatively, the output terminal of low-pass filter
180 is connected to the input terminal of alignment control system
75.
[0033] Reference is now made to Fig. 5, which is a table comparing the system of Fig. 4
to a signal strength system of polarization alignment. Following is an algebraic treatment
comparing the autocorrelation method using autocorrelation apparatus
65 of Fig. 4 to the traditional signal-strength system of polarization alignment. It
should be noted that the following algebraic treatment is presented to facilitate
a more complete understanding of the system of Fig. 4 and is not in any way limiting
the scope of the invention as defined by the claims appended hereto.
[0034] At optimal alignment of the antenna polarization axes
25, 30 towards satellite
20 the level of output
185 is zero. At a small error rotation angle Δθ from optimum polarization alignment the
signal to noise ratio of output
185 relative to a maximum signal to noise ratio of output
185 obtained with an offset angle of 45° is given by:

where [S/N]
(DC)(Δ θ) is the signal to noise ratio of output
185 due to an error rotation angle of Δθ and [S/N]
(DC)(45°) is the signal to noise ratio of output
185 due to an error rotation angle of 45°) and ≈ means approximately equal to.
[0035] At the output of band-pass filter
120 the following equation is valid:

where [S/N]
(IF Co-Pol)(45°) is the signal to noise ratio of output
130 information bandwidth at offset rotation angle of 45°, [SIN](0°)
(IFCo-Pol) is the signal to noise ratio of output
130 information bandwidth at offset rotation angle of 0° and 3dB
(45°) denotes a reduction in the signal to noise ratio by 3dB due to a rotation angle of
45°.
[0036] The following equation is also valid:

where DW is the signal bandwidth of output
130, DW1 is the bandwidth of band-pass filter
120 and DW2 is the bandwidth of low-pass filter
180 and

where 3dB
(Mixer) is the reduction in the signal to noise ratio by 3dB due to an insertion loss of
mixer
165.
[0037] Substituting equation 4 into equation 3 gives:

[0038] The following algebraic relationship is valid:

[0039] Equation 6 can be rearranged to give:

[0040] As mentioned above with relation to Fig. 4, the bandwidth of band-pass filter
120 is typically in the range 6 MHz to 8 MHz therefore:

[0041] Now, assuming a worst case of DW/DW1 = 0.1 = -10dB, then:

[0042] Now, assuming a worst case of [S/N]
(IF Co.Pol)(0°) = 10dB and substituting equation 9 into equation 5, gives:

Equation 1 is rearranged giving:

Therefore, by substituting equation 11 into equation 10, assuming a worse case scenario
the signal to noise ratio of output
185 due to an error rotation angle of Δθ is given by:

As the practical threshold level for error detection in the polarization alignment
is a signal to noise ratio of 1 to I, which is 0dB, then for the traditional polarization
alignment method, based on received satellite signal strength alone, the relative
change above threshold due to a small offset rotation angle of Δθ is given by approximately:

[0043] Therefore, it can be seen that the autocorrelation method results in more than 40dB
increase in the signal to noise ratio as compared to the traditional signal-strength
pointing method. The results are shown in the table of Fig. 5. The second column of
the table represents the results of the autocorrelation method based on equation 12
and the third column of the table represents the results of the traditional signal-strength
pointing method based on equation 13.
[0044] Reference is now made to Fig. 6, which is a schematic representation of the operation
of alignment control system
75 for use with the autocorrelation apparatus
65. In block
190, output
185 being the result of autocorrelation is processed. This process includes checking
an autocorrelation result storage area
195 for a prior stored result of autocorrelation. If there is no prior stored result
of autocorrelation, the processor decides on an initial estimated adjustment command
for alignment actuator
80. The process continues with block
200. In block
200, new data is stored. Newly received result of autocorrelation is stored in autocorrelation
result storage area
195. The initial adjustment command for alignment actuator
80 is stored in an actuator command storage area
205. In block
210, an actuator controller sends the initial adjustment command to alignment actuator
80. Alignment actuator
80 adjusts polarization axes
25, 30.
[0045] After the initial adjustment has been made a new result of autocorrelation is received.
The process continues at block
190. In block
190, autocorrelation result storage area
195 is checked for a prior stored result of autocorrelation. The prior stored result
is retrieved and compared to the newly received result of autocorrelation. If the
new result is less than the prior result, alignment actuator
80 will be instructed to continue adjusting in the same direction. If the new result
is greater than the prior result, alignment actuator
80 will be instructed to adjust in an opposing direction. The prior actuator command
is retrieved from actuator command storage area
205. A new actuator adjustment command is calculated. The process continues with block
200. In block
200, new data is stored. The newly received result of autocorrelation is stored in autocorrelation
result storage area
195. The new adjustment command is stored in an actuator command storage area
205. In block
210, actuator controller sends the new adjustment command to alignment actuator
80. Alignment actuator
80 adjusts polarization axes
25, 30. This process continues repeatedly at block
190 until output
185 being the result of autocorrelation approaches zero.
1. A method for aligning antenna (17) polarization axes (25, 30) of a dual polarized
end-user terminal (10) having an antenna (17), the antenna (17) being aligned toward
a satellite (20) in relation to azimuth and elevation, the end-user terminal (10)
being configured to produce a first output (40) corresponding to a first component
(45) of a received signal (15) parallel to a first polarization axis (25) of the antenna
(17) and a second output (50) corresponding to a second component (55) of the received
signal (15) parallel to a second polarization axis (30) of the antenna (17), the first
polarization axis (25) being orthogonal to the second polarization axis (30), the
method comprising the steps of:
(a) receiving a linearly polarized signal (15) having a frequency wherein for said
frequency and during a time period when said signal (15) is being transmitted, the
satellite (20) is not transmitting signals with a linear polarization that is orthogonal
to said linearly polarized signal (15);
(b) autocorrelating the first output (40) and the second output (50) to produce a
measurement of autocorrelation by inputting said first output (40) and said second
output (50) into an electronic mixer (165) and inputting the output of said electronic
mixer (165) into a low-pass filter (180) to produce said measurement of autocorrelation;
and
(c) adjusting the antenna (17) polarization axes (25, 30) to minimize said measurement
of autocorrelation.
2. The method of claim 1 further comprising the step of reducing proportionately frequencies
of said first output (40) and said second output (50).
3. The method of claim 2 further comprising the step of tuning said first output (40)
and said second output (50) to said frequency.
4. The method of claim 2 further comprising the step of filtering said first output (40)
using a first band pass filter (120) and said second output (50) using a second band
pass filter (125).
5. The method of claim 1 further comprising, after said step of autocorrelating, the
step of displaying said measurement of autocorrelation.
6. The method of claim 1 wherein said step of adjusting is performed by actuating an
alignment actuator (80) configured to adjust the antenna polarization axes (25, 30)
to minimize said measurement of autocorrelation.
7. A system for aligning antenna polarization axes (25, 30) of a dual polarized end-user
terminal (10) having an antenna (17), the antenna (17) being aligned toward a satellite
(20) in relation to azimuth and elevation, the end-user terminal (10) being configured
to produce a first output (40) corresponding to a first component (45) of a received
signal (15) parallel to a first polarization axis (25) of the antenna (17) and a second
output (50) corresponding to a second component (55) of the received signal (15) parallel
to a second polarization axis (30) of the antenna (17), the first polarization axis
(25) being orthogonal to the second polarization axis (30), the system comprising:
(a) a first connection configured for connection to the end-user terminal (10) for
receiving the first output (40);
(b) a second connection configured for connection to the end-user terminal (10) for
receiving the second output (50); and
(c) an autocorrelation apparatus (65) having a first input and a second input; wherein
said first connection is connected to said first input and said second connection
is connected to said second input, said autocorrelation apparatus (65) further including
a low-pass filter (180) having an input, and an electronic mixer (165) having a first
input that is connected to said first connection, a second input that is connected
to said second connection and an output that is connected to said input of said low-pass
filter (180).
8. The system of claim 7, further comprising a display (70) having an input and wherein:
(a) said low-pass filter (180) has an output; and
(b) the input of a display is connected to said output of said low-pass filter (180).
9. The system of claim 7, wherein:
(a) said autocorrelation apparatus (65) further includes a dual polarized block down-converter
having a first input (40) that is connected to said first connection and a second
input (50) that is connected to said second connection; and
(b) said dual polarized block down-converter is interposed between said first connection,
said second connection and said electronic mixer (165).
10. The system of claim 7, wherein said autocorrelation apparatus (65) further includes:
(a) a first down-converter (85) that is interposed between said first connection and
said electronic mixer (165); and
(b) a second down-converter that is interposed between said second connection and
said electrode mixer (165).
11. The system of claim 7, wherein said autocorrelation apparatus (65) includes:
(a) a first tuner (100) that is interposed between said first connection and said
electronic mixer (165); and
(b) a second tuner (105) that is interposed between said second connection and said
electronic mixer (165).
12. The system of claim 7, wherein said autocorrelation apparatus (65) includes:
(a) a first band pass filter (120) that is interposed between said first connection
and said electronic mixer (165); and
(b) a second band pass filter (125) that is interposed between said second connection
and said electronic mixer (165).
13. The system of claim 7, further comprising an alignment control system (75) and an
alignment actuator (80) wherein said alignment control system (75) is configured to
control said alignment actuator (80) to adjust the antenna (17) polarization axes
(25, 30) in response to an output of said autocorrelation apparatus (65).
1. Ein Verfahren zur Ausrichtung von Antennen (17)- Polarisierungsachsen (25, 30) einer
doppelpolarisierten Endbenutzer-Station (10), die eine Antenne (17) hat, wobei die
Antenne (17) im Hinblick auf Azimut und Elevation auf einen Satelliten (20) ausgerichtet
wird, wobei die Endbenutzer-Station (10) ausgebildet ist, um eine erste Ausgabe (40)
zu erzeugen, die einer ersten Komponente (45) eines empfangenen Signals (15), parallel
zu einer ersten Polarisierungsachse (25) der Antenne (17), entspricht, und um eine
zweite Ausgabe (50) zu erzeugen, die einer zweiten Komponente (55) des empfangenen
Signals (15), parallel zu einer zweiten Polarisierungsachse (30) der Antenne (17),
entspricht, wobei die erste Polarisierungsachse (25) orthogonal zur zweiten Polarisierungsachse
(30) ist, wobei das Verfahren folgende Schritte umfaßt:
(a) Empfang eines linear polarisierten Signals (15) mit einer Frequenz, worin für
diese Frequenz und während eines Zeitraums, wenn das Signal (15) übertragen wird,
der Satellit (20) Signale mit einer linearen Polarisierung, die orthogonal zum linear
polarisierten Signal (15) ist, nicht überträgt;
(b) Autokorrelation der ersten Ausgabe (40) und der zweiten Ausgabe (50), um eine
Messung der Autokorrelation zu erzeugen, durch Eingabe der ersten Ausgabe (40) und
der zweiten Ausgabe (50) in einen elektronischen Mischer (165) und Eingeben der Ausgabe
des elektronischen Mischers (165) in einen Tiefpaßfilter (180), um die Messung der
Autokorrelation zu erzeugen; und
(c) Einstellen der Antennen (17)-Polarisierungsachsen (25, 30), um die Messung der
Autokorrelation zu minimieren.
2. Das Verfahren von Anspruch 1, das weiter den Schritt der proportionalen Reduzierung
der Frequenzen der ersten Ausgabe (40) und der zweiten Ausgabe (50) umfaßt.
3. Das Verfahren von Anspruch 2, das weiter den Schritt des Abstimmens der ersten Ausgabe
(40) und der zweiten Ausgabe (50) auf die Frequenz umfaßt.
4. Das Verfahren von Anspruch 2, das weiter den Schritt des Filterns der ersten Ausgabe
(40) mit Hilfe eines ersten Bandpassfilters (120) und der zweiten Ausgabe (50) mit
Hilfe eines zweiten Bandpassfilters (125) umfaßt.
5. Das Verfahren von Anspruch 1, das weiter nach dem Schritt der Autokorrelation den
Schritt des Anzeigens der Autokorrelationsmessung umfaßt.
6. Das Verfahren von Anspruch 1, worin der Schritt des Einstellens durchgeführt wird
durch Betätigung eines Ausrichtungs-Aktuators (80), der ausgebildet ist, um die Antennen-Polarisierungsachsen
(25, 30) einzustellen, um die Messung der Autokorrelation zu minimieren.
7. Ein System zur Ausrichtung von Antennen-Polarisierungsachsen (25, 30) einer doppelpolarisierten
Endbenutzer-Station (10), die eine Antenne (17) hat, wobei die Antenne (17) im Hinblick
auf Azimut und Elevation auf einen Satelliten (20) ausgerichtet ist, wobei die Endbenutzer-Station
(10) ausgebildet ist, um eine erste Ausgabe (40) zu erzeugen, die einer ersten Komponente
(45) eines empfangenen Signals (15), parallel zu einer ersten Polarisierungsachse
(25) der Antenne (17), entspricht, und um eine zweite Ausgabe (50) zu erzeugen, die
einer zweiten Komponente (55) des empfangenen Signals (15), parallel zu einer zweiten
Polarisierungsachse (30) der Antenne (17), entspricht, wobei die erste Polarisierungsachse
(25) orthogonal zur zweiten Polarisierungsachse (30) ist, wobei das System folgendes
umfaßt:
(a) eine erste Verbindung, ausgebildet zur Verbindung mit der Endbenutzer-Station
(10), um die erste Ausgabe (40) zu empfangen;
(b) eine zweite Verbindung, ausgebildet zur Verbindung mit der Endbenutzer-Station
(10), um die zweite Ausgabe (50) zu empfangen; und
(c) eine Autokorrelationsvorrichtung (65) mit einer ersten Eingabe und einer zweiten
Eingabe, worin die erste Verbindung mit der ersten Eingabe verbunden ist und die zweite
Verbindung mit der zweiten Eingabe verbunden ist, wobei die Autokorrelationsvorrichtung
(65) weiter einen Tiefpassfilter (180) mit einer Eingabe einschließt und einen elektronischen
Mischer (165) mit einer ersten Eingabe, die mit der ersten Verbindung verbunden ist,
einer zweiten Eingabe, die mit der zweiten Verbindung verbunden ist, und einer Ausgabe,
die mit der Eingabe des Tiefpassfilters (180) verbunden ist.
8. Das System von Anspruch 7, das weiter eine Anzeige (70) mit einee Eingabe umfaßt und
worin:
(a) der Tiefpassfilter (180) eine Ausgabe hat; und
(b) die Eingabe einer Anzeige mit der Ausgabe des Tiefpassfilters (180) verbunden
ist.
9. Das System von Anspruch 7, worin:
(a) die Autokorrelationsvorrichtung (65) weiter einen doppelpolarisierten Block-Abwärtsumsetzer
mit einer ersten Eingabe (40) einschließt, die mit der ersten Verbindung verbunden
ist, und einer zweite Eingabe (50), die mit der zweiten Verbindung verbunden ist;
und
(b) der doppelpolarisierte Block-Abwärtsumsetzer zwischen der ersten Verbindung, der
zweiten Verbindung und dem elektronischen Mischer (165) angeordnet ist.
10. Das System von Anspruch 7, worin die Autokorrelationsvorrichtung (65) weiter folgendes
einschließt:
(a) einen ersten Abwärtsumsetzer (85), der zwischen der ersten Verbindung und dem
elektronischen Mischer (165) angeordnet ist; und
(b) einen zweiten Abwärtsumsetzer, der zwischen der zweiten Verbindung und dem elektronischen
Mischer (165) angeordnet ist.
11. Das System von Anspruch 7, worin die Autokorrelationsvorrichtung (65) folgendes einschließt:
(a) einen ersten Empfänger (100), der zwischen der ersten Verbindung und dem elektronischen
Mischer (165) angeordnet ist; und
(b) einen zweiten Empfänger (105), der zwischen der zweiten Verbindung und dem elektronischen
Mischer (165) angeordnet ist.
12. Das System von Anspruch 7, worin die Autokorrelationsvorrichtung (65) folgendes einschließt:
(a) einen ersten Bandpassfilter (120), der zwischen der ersten Verbindung und dem
elektronischen Mischer (165) angeordnet ist; und
(b) einen zweiten Bandpassfilter (125), der zwischen der zweiten Verbindung und dem
elektronischen Mischer (165) angeordnet ist.
13. Das System von Anspruch 7, das weiter ein Ausrichtungs-Steuersystem (75) und einen
Ausrichtungs-Aktuator (80) umfaßt, worin das Ausrichtungs-Steuersystem (75) ausgebildet
ist, um den Ausrichtungs-Aktuator (80) zu steuern, um die Antennen (17)-Polarisierungsachsen
(25, 30) als Reaktion auf eine Ausgabe der Autokorrelationsvorrichtung (65) einzustellen.
1. Procédé pour aligner des axes de polarisation (25,30) d'une antenne (17) d'un terminal
(10) d'un utilisateur final à double polarisation et ayant une antenne (17), l'antenne
(17) étant alignée vers un satellite (20) selon un azimut et une élévation, le terminal
(10) de l'utilisateur final étant configuré pour produire une première sortie (40)
correspondant à une première composante (45) d'un signal reçu (15) parallèle à un
premier axe de polarisation (25) de l'antenne (17) et une seconde sortie (50) correspondant
à une seconde composante (55) du signal reçu (15) parallèle à un second axe de polarisation
(30) de l'antenne (17), le premier axe de polarisation (25) étant orthogonal au second
axe de polarisation (30), le procédé comprenant les deux étapes de :
a) recevoir un signal polarisé linéairement (15) et ayant une fréquence dans laquelle
pour ladite fréquence et pendant une période où ledit signal (15) est en cours de
transmission, le satellite (20) ne transmet pas des signaux avec une polarisation
linéaire qui est orthogonale audit signal polarisé linéairement (15) ;
b) autocorréler la première sortie (40) et la seconde sortie (50) pour produire une
mesure d'autocorrélation en appliquant ladite première sortie (40) et ladite deuxième
sortie (50) sur un mixeur électronique (165) et en appliquant la sortie dudit mixeur
électronique (165) sur un filtre passe-bas (180) pour produire ladite mesure d'autoborrélation
; et
c) ajuster les axes de polarisation (25,30) de l'antenne (17) pour minimiser ladite
mesure d'auto corrélation.
2. Procédé selon la revendication 1 comprenant en outre l'étape de réduction proportionnelle
des fréquences de ladite première sortie (40) et de ladite deuxième sortie (50).
3. Procédé selon la revendication 2 comprenant en outre l'étape consistant à accorder
ladite première sortie (40) et ladite deuxième sortie (50) à ladite fréquence.
4. Procédé selon la revendication 2 comprenant en outre l'étape de filtrage de ladite
première sortie (40) en utilisant un premier filtre passe bande (120) et ladite deuxième
sortie (50) en utilisant un second filtre passe bande (125).
5. Procédé selon que la revendication 1, comprenant en outre, après ladite étape d'autocorrélation,
l'étape d'affichage de ladite mesure d'autocorrélation.
6. Procédé selon la revendication 1, dans lequel ladite étape d'ajustement est réalisée
en actionnant un actionneur d'alignement (80) configuré pour ajuster les axes de polarisation
de l'antenne (25,30) pour minimiser ladite mesure d'auto corrélation.
7. Système pour aligner des axes de polarisation (25,30) d'une antenne d'un terminal
(10) à double polarisation d'un utilisateur final ayant une antenne (17), l'antenne
(17) étant alignée vers un satellite (20) selon un azimut et une élévation, le terminal
(10) d'utilisateur final étant configuré pour produire une première sortie (40) correspondant
à une première composante (45) d'un signal reçu (15) parallèle à un premier axe de
polarisation (25) de l'antenne (17) et une deuxième sortie (50) correspondant à une
deuxième composante (55) du signal reçu (15) parallèle à un deuxième axe de polarisation
(30) de l'antenne (17), le premier axe de polarisation (25) étant orthogonal au deuxième
axe de polarisation (30), le système comprenant :
a) une première connexion configurée pour connecter le terminal (10) de l'utilisateur
final pour recevoir la première sortie (40) ;
b) une deuxième connexion configurée pour connecter le terminal (10) de l'utilisateur
final pour recevoir la deuxième sortie (50); et
c) un d'appareil d'autocorrélation (65) ayant une première entrée et une deuxième
entrée, dans lequel ladite première connexion est connectée à ladite première entrée
et ladite deuxième connexion est connectée à ladite deuxième entrée, ledit appareil
d'autocorrélation (65) incluant en outre un filtre passe bas (180) ayant une entrée,
et un mixeur électronique (165) ayant une première entrée qui est connectée à ladite
première connexion, une deuxième entrée qui est connectée à ladite deuxième connexion
et une sortie qui est connectée à ladite entrée dudit filtre passe-bas (180).
8. Système selon la revendication 7, comprenant en outre un afficheur (70) ayant une
entrée et dans lequel :
a) ledit filtre passe bas (180) a une sortie ; et
b) l'entrée d'un afficheur est connectée à ladite sortie dudit filtre passe bas (180).
9. Système selon la revendication 7, dans lequel :
a) ledit appareil d'autocorrélation (65) comprend en outre un convertisseur abaisseur
de fréquence en bloc à double polarisation ayant une première entrée (40) qui est
connectée à ladite première connexion et une deuxième entrée (50) qui est connectée
à ladite deuxième connexion ; et
b) ledit convertisseur abaisseur de fréquence en bloc à double polarisation est interposé
entre ladite première connexion, ladite deuxième connexion et ledit mixeur électronique
(165).
10. Système selon la revendication 7, dans lequel ledit appareil d'autocorrélation (65)
comprend en outra :
a) un premier convertisseur abaisseur de fréquence (85) qui est interposé entre ladite
première connexion et ledit mixeur électronique (165) ; et
b) un deuxième convertisseur abaisseur de fréquence qui est interposé entre ladite
deuxième connexion et ledit mixeur électronique (165).
11. Système selon la revendication 7, dans lequel ledit appareil d'autocorrélation (65)
inclut:
a) un premier syntoniseur (100) qui est interposé entre ladite première connexion
et ledit mixeur électronique (165) ; et
b) un deuxième syntoniseur (105) qui est interposé entre ladite deuxième connexion
et ledit mixeur électronique (165).
12. Système selon la revendication 7, dans lequel ledit appareil d'autocorrélation (65)
inclut :
a) un premier filtre passe bande (120) qui est interposé entre ladite première connexion
et ledit mixeur électronique (165) ; et
b) un deuxième filtre passe bande (125) qui est interposé entre ladite deuxième connexion
et ledit mixeur électronique (165).
13. Système selon la revendication 7, comprenant en outre un système de contrôle d'alignement
(75) et un actionneur d'alignement (80) dans lequel ledit système de contrôle d'alignement
(75) est configuré pour contrôler ledit actionneur d'alignement (80) pour ajuster
les axes de polarisation (25,30) de l'antenne (17) en réponse à une sortie dudit appareil
d'autocorrélation (65).